DocumentCode
518400
Title
Notice of Retraction
Automatic thrust augmentation
Author
Balaji, S. ; Dinesh, M. ; Raj, N Dileep
Author_Institution
Aeronaut. Eng. Dept., Rajalakshmi Eng. Coll., Chennai, India
Volume
5
fYear
2010
fDate
16-18 April 2010
Abstract
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
The automatic thrust augmentation is the method of powering a high speed aircraft with the objective of minimizing the fuel consumption and making use of the atmospheric air in collecting the propellant. The automatic thrust augmentation is a system that can be used in assisting the main engine in order to provide thrust during critical situations which includes crossing the sonic region, during air combat, taking off from an aircraft carrier and so on. This method of thrust augmentation includes making use of the atmospheric air in collecting the propellant (oxidizer) and mixing it with the aircraft´s fuel for the combustion to take place. Also, these processes occur automatically without pilots´ effort which also increases accuracy and relieves pilot´s stress. Since we are collecting the propellant from atmosphere, we can minimise fuel consumption significantly, and further research in this can lead to many other developments in aerospace field. We have given a conceptual idea on extracting the propellant from atmosphere and on providing automatic thrust augmentation.
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
The automatic thrust augmentation is the method of powering a high speed aircraft with the objective of minimizing the fuel consumption and making use of the atmospheric air in collecting the propellant. The automatic thrust augmentation is a system that can be used in assisting the main engine in order to provide thrust during critical situations which includes crossing the sonic region, during air combat, taking off from an aircraft carrier and so on. This method of thrust augmentation includes making use of the atmospheric air in collecting the propellant (oxidizer) and mixing it with the aircraft´s fuel for the combustion to take place. Also, these processes occur automatically without pilots´ effort which also increases accuracy and relieves pilot´s stress. Since we are collecting the propellant from atmosphere, we can minimise fuel consumption significantly, and further research in this can lead to many other developments in aerospace field. We have given a conceptual idea on extracting the propellant from atmosphere and on providing automatic thrust augmentation.
Keywords
aerospace engines; aerospace propulsion; aerospace field; aircraft carrier; automatic thrust augmentation; engine; high speed aircraft; Aircraft propulsion; Atmosphere; Combustion; Cryogenics; Engines; Fuels; Level control; Magnetic liquids; Oxygen; Refrigeration; minimising fuel consumption; propellant extraction from atmosphere; thrust augmentation;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Engineering and Technology (ICCET), 2010 2nd International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4244-6347-3
Type
conf
DOI
10.1109/ICCET.2010.5486136
Filename
5486136
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